TY - JOUR AU - Kravchuk, I.S. AU - Dmytro, Bashynskyi AU - Taranenko, V.V. AU - Zirka, M.V. PY - 2021/09/28 Y2 - 2024/03/28 TI - Flight Range Extension of a Guided Aerial Bomb with a Rocket Engine during Climb Bombing JF - Advances in Military Technology JA - AiMT VL - 16 IS - 2 SE - Research Paper DO - 10.3849/aimt.01462 UR - https://aimt.cz/index.php/aimt/article/view/1462 SP - 265-276 AB - <p>The possibility of a significant flight range extension of a guided aerial bomb during climb bombing due to the jet thrust created by a solid-propellant rocket engine was considered. By means of simulation, a comparative analysis of the range of a guided aerial bomb equipped (not equipped) with a solid-propellant rocket engine under typical flight conditions of the carrier aircraft during level flight and climb bombing was performed. It was demonstrated that the use of a solid-propellant rocket engine, whose mass is 20 % of the guided aerial bomb’s mass, allows to increase the horizontal range of its flight at least twice.</p><p> </p> ER -